US3099455A - Piston ring assembly - Google Patents
Piston ring assembly Download PDFInfo
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- US3099455A US3099455A US57040A US5704060A US3099455A US 3099455 A US3099455 A US 3099455A US 57040 A US57040 A US 57040A US 5704060 A US5704060 A US 5704060A US 3099455 A US3099455 A US 3099455A
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- ring
- cylindrical wall
- apertures
- coil spring
- piston ring
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- 239000002184 metal Substances 0.000 claims description 6
- 238000010276 construction Methods 0.000 description 7
- 230000004048 modification Effects 0.000 description 7
- 238000012986 modification Methods 0.000 description 7
- 230000006835 compression Effects 0.000 description 6
- 238000007906 compression Methods 0.000 description 6
- 125000006850 spacer group Chemical group 0.000 description 5
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 230000008602 contraction Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/061—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging using metallic coiled or blade springs
- F16J9/062—Coiled spring along the entire circumference
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/061—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging using metallic coiled or blade springs
- F16J9/063—Strip or wire along the entire circumference
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/064—Rings with a flat annular side rail
- F16J9/066—Spring expander from sheet metal
- F16J9/069—Spring expander from sheet metal with a "C"-shaped cross section along the entire circumference
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/12—Details
- F16J9/14—Joint-closures
- F16J9/145—Joint-closures of spring expanders
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
July 30, 1963 G. c. MAYFIELD PISTON RING ASSEMBLY Filed Sept. 19, 1960 2 Sheets-Sheet 1 FIG.
INVENTOR. GEORGE C. MAYFIELD ATTORNEYS United States Patent 3,099,455 PHSTGN RTNG ASSEMBLY George C. Mayfield, Richmond Heights, Mo., assignor to McQuay-Norris Manufacturing Company, St. Louis, Mo., a corporation of Delaware Filed Sept. 19, 1960, Ser. No. 57,040 2 Claims. (Cl. 277-163) This invention relates to multi-piece piston ring assemblies and more specifically to the type of piston ring assembly in which split piston rings or rails are supported in axially spaced relation in a piston ring groove by a split backing ring or spacer ring and in which a radial control force is applied to the piston rings or rails by an annular coil spring held compressed inside the backing ring or spacer ring. Such a piston ring assembly is shown in my co-pending application for Piston Ring Assemblies Serial No. 56,223, filed September 15, 1960, now Patent No. 3,080,172, our docket No. 277. The instant invention disclosed in this application is directed specifically to a backing ring construction which is distinctly different in operation and result. The piston ring assembly, hereinafter described in detail, is primarily intended for use as an oil control ring on a piston for an internal combustion piston engine, but, of course, the assembly described is merely exemplary, and it is contemplated that the assembly may include rings designed for other purposes.
According to this invention, this piston ring assembly is full-floating and non-bottoming in the piston ring groove and includes split expansible and contractible piston ring elements of suitable design supported in the ring groove of the piston in spaced relation by a novel form of backing ring or spacer ring element. This backing ring or spacer ring element is split to permit expansion and limited contraction. The backing ring element is an annular strip of spring metal with a channel shaped cross-section providing a cylindrical wall or web and annular diametrically inwardly directed flanges or legs at opposite edges of the cylindrical wall. At the inner periphery of each annular flange or leg are upstanding rims extending oppositely and outwardly of the backing ring to engage the inner periphery of the piston rings when supported between the outer surface of the annular flanges or legs and the inner radial face of the piston ring groove. A radially outwardly directed resilient force is applied to the cylindrical wall of the backing ring by a plain round coil spring with a pre-selected free length formed into an annulus by means holding the opposite ends of the coil spring in abutting relation. In accordance with usual practice, the free length of the annular coil spring is greater than the inner circumference of the cylindrical wall of the backing ring when this ring is in operating relationship with the piston ring engaging a cylinder wall, and, consequently, the annular coil spring is compressed circumferentially so that it exerts a continuous expansive force radially outwardly on the cylindrical inner wall of the backing ring, which force is uniform around the inner periphery of the cylindrical wall of the backing ring. Like radially outwardly directed forces are transposed from the backing ring to the piston ring through the upstanding rims.
As set forth in my prior application above referred to, it is desirable to obtain a circumferentially uniformly distributed expansive force acting on the piston ring from the annular coil spring. This result may be obtained by a ring assembly, which acts as a whole, and a backing ring in particular which has suflicient flexibility to accommodate the very small variations in cylinder wall contour from true cylindrical shape. In addition, sliding friction between the ring elements in the ring assembly must be held to a minimum especially at the bearing surfaces between the cylindrical wall of the backing ring and the annular coil spring. In my prior application, the first re- "ice quirement, flexibility, is obtained in a similar manner as in the ring shown in my prior Patent 2,486,359 of October 25, 1949, and friction is minimized by inclining the slots in the cylindrical wall with respect to the axis of the backing ring in a direction opposite to the lay of the wire in the coils at the bearing surfaces between the cylindrical wall of the backing ring and the coil.
There are applications for piston ring assemblies in which greater and more uniform beam strength is required in the channel shaped backing ring than can be provided by any change in spacing or width of the slots in a slotted ring. The instant invention provides this characteristic while maintaining the desirable characteristic of uniform circumferential flexibility provided by the slotted ring. Thus, according to this invention, semi-elliptical apertures are formed alternately in opposite edges of the backing ring and extend from within the flanges or leg portions to within the cylindrical wall or web portion. 'In other words, the straight edge of the semi-elliptical aperture is located in the flange, and the curved edge extends either to or slightly beyond the middle of the cylindrical wall or web. The alternate locations of these spaced apertures, extending as they do from opposite edges of the ring, leave a sinuous strip of substantially uniform cross-section forming the cylindrical wall or web, or what might be considered as diagonal web members in the cylindrical wall, alternately inclined in opposite directions in a trusslike manner. These truss-like members or webs are interconnected between the edges of the cylindrical wall. Since the apertures extend across the corner bends of the channel between the flange and the cylindrical wall thereof, the rigidity of the backing ring to circumferential flexibility inherent in the angular relation of the channel is avoided. The backing ring becomes flexible, but maintains its beam strength due to the truss-like formation in the cylindrical wall.
The second requirement, minimum sliding friction, especially at the bearing surfaces between the backing ring and the annular coil spring is obtained inmuch the same way as disclosed in my prior application above identified. In other words, coil diameter in the annular spring is such that the spring can roll on the cylindrical wall of the backing ring and is definitely not confined against axial movement between the flanges. The trusslike interconnected webs forming the cylindrical wall, which are formed by the alternate arrangement of semielliptical apertures, have edges on one side which are inclined in a direction opposite to the lay of the wire in the coils of the coil spring at the bearing surfaces between the cylindrical wall of the backing ring and the coil spring. Opposite edges of these webs have a greater inclination in the same direction as the lay of the coils at the bearing surface between the cylindrical wall of the backing ring and the coil spring. This construction eliminates interference between the coils of the spring and the edges of the truss-like web. It might be added, however, that the wire size chosen for the coil spring is relatively large with respect to the coil size, thus, providing for substantial circumferential rigidity. Together, these features contribute to obtaining minimum friction between coil spring and cylindrical wall during relative circumferential movement of one with respect to the other and maximum uniformity of the control pressure over the surface of the cylindrical wall. The coil spring is perrnitted to float between the flanges of the backing ring and seek a path of minimum frictional contact therewith.
It is an object of this invention to provide a piston ring assembly in which radially directed forces are uniform between the piston rings and the cylinder walls.
It is another object of this invention to provide a back- 3 ing ring in a piston ring assembly which has uniform flexibility and substantial beam strength.
It is still another object of this invention to provide a backing ring in a piston ring assembly which has high beam strength and yet uniform circumferential flexibility in a radial direction.
It is still another object of this: invention to provide a backing ring in a piston ring assembly which has a discontinuous cylindrical wall confining a coil expansion spring.
It is still another object of this invention to provide in the organization above described broadly the maximum of flexibility with beam strength and the minimum of friction and interference between spring and backing rlng.
Further objects and advantages of this invention will appear from the following which is a full, clear and exact description of the invention when taken with the accompanying drawings forming a part thereof and in which:
FIG. 1 is a plan view of a punched spring strip of metal from which one of the ring elements of the piston ring assembly is formed;
FIG. 2 and FIG. 3 are elevational and cross-sectional views of the strip shown in FIG. 1 after it has been formed into a channel suitable for a backing ring;
FIG. 4 is a top plan view of a backing ring formed from the channel shown in FIGS. 2 and 3;
FIG. 5 is a top plan view of an annular coil compression spring used as an expander for the backing ring shown in FIG. 4;
FIG. 6 is an enlarged detailed view of the connector for the ends of the coil spring shown in FIG. 5;
FIG. 7 is a perspective view of a piston ring assembly formed from the parts shown in FIGS. 2 through 6, inelusive;
FIGS. 8 through 13 are enlarged detailed views illustrating different forms of connectors for the end of a coil spring which may be used in place or substitution for the connectors shown in FIG. 6; and
FIG. 14 is a transverse section through a portion of a piston, cylinder Wall and piston ring on an enlarged scale illustrating the use of the backing ring in a different ring assembly.
The following is a detailed description of the construction shown in the several views of the drawings. The manner in which the construction shown therein is described does not necessarily correspond with the method of manufacture, but is chosen here merely for the purposes of convenience to facilitate an explanation of the invention. The strip of spring steel 10, shown in FIG. 1, is chosen of proper width to form the complete channel member for the backing ring in this piston ring assembly, and the phantom lines AA and BB, shown in FIG. 1, illustrate the future location of the corner bends to form the channel. These are placed on FIG. 1 to indicate the location of the apertures 11, 12, 13, 14, etc., which are punched in the spring strip 10. Likewise, the phantom line (3-0 indicates the center between the lines AA and BB and also indicates the depth to which the apertures 11, 12, 13, 14 and 15 extend into what will be the cylindrical wall of the backing ring. Phantom lines D-D and BE indicate the location of the corner bend in the strip which will form the upstanding rim on the channel. Each of the apertures 11 through 15, etc., have straight edges 21 through 25, inclusive, which are displaced outwardly of the lines AA and BB from the center of the strip. These straight edges 21, 23, 25 will be located in the lower flange of the channel between the lines BB and E-E while the straight edges 22, 24, etc., will be located in the upper flange of the channel since they are between the lines AA and BB. Each of the apertures 11 through 15 punched into the strip 10 also have semi-elliptical shaped edges extending toward the center of the strip 10 and indicated as 31 through 35, inclusive.
Referring now to FIGS. 2 and 3, the strip 10 with the apertures so formed is rolled into a channel section. The channel will have a wall or Web portion 1 and upper and lower flanges 2 and 3 which have formed at their ends the rims 4 and 5. A will be apparent from an inspection of these figures, the apertures 11 15, inclusive, are now located so that the straight edges thereof, '21 through 25, are located in the flanges 2 and 3, Whereas the elliptical edges 31 through 35 are located in the wall 1. Since the apertures 11 through .15, inclusive, extend across the corners of the channel, indicated by the lines BB and E-E of FIG. 1, the inherent rigidity which would be imparted by the corner bends to the flange strip 10 is avoided, and the strip 10 becomes flexible longitudinally. The apertures .11 through r15, inclusive, etc., located as they are alternately at the upper and lower edges of the wall 1 of the strip 10 form, as it were, a plurality of inclined struts for a truss-like structure. To ilustrate an understanding, the phantom lines FF have been drawn on FIG. 2 which indicate the center line of each strut in the truss-like structure of the cylindrical wall 1. Also indicated in \FIG. 2. is a mean cross-section of the strip of material torming the cylindrical wall .1. This is represented by the sinuous curved phantom line G-G which is drawn through the points of mean cross-section. The apertures 11 through 15, inclusive, etc., along the strip are so arranged and proportioned that the widthwise dis tance indicated by the sinuous curved phantom line GG is substantially the same along the length of the strip 10. This peculiar arrangement, propo-ntioning and orientation of the apertures 11 through 15, etc., inclusive, produces a strip of metal between the flanges 2 and 3 in the wall 1 which will be of uniform strength and springiness in the plane of bending parallel with the flanges 2 and 3. On the other hand, the channel 10 will retain its beam strength and its resistance to distortion in planes parallel with the web portion 1. In the latter respect, it differs from all prior art constructions.
The strip 10 which has been formed into a channel is then rolled, or otherwise formed into rings 40, such as shown in FIG. 4, with spaced ends 41 and 42. This forming operation makes an annular ring from the strip 10, which ring has its cylindrical wall 1 disposed at its outer periphery and the flanges 2 and 3 projecting radially inwardly therefrom. Rims 4 and 5 will then project axially of the ring 40.
This ring 40 is adapted to contain a coil compression spring 50, such as shown in 'FIG. 5. The coil spring 50 is of relatively conventional construction formed of spaced helical coils of spring wire. The ratio of wire size relative to coil size is chosen to be relatively large tor reasons which will appear hereinafter. Opposite ends 51 and 52 of the coil spring 50 are held in abutting relation by a connector 55, as in FIG. 6. Each end 56' and 57 of the connector is preferably curved so as to telescope within the coils of the coil spring 50. The center portion 58 is formed into a helical loop and acts as an abutment between the ends 51 and S2 of the coil spring 50.
FIG. 7 illustrates the operative relationship between all of the parts of the piston ring assembly. In this 'view, the upper and lower flanges 2 and 3 of the backing ring 40 act as supports and spacers for a pair of split annular rails 60 and '61, the outer peripheries of which bear against the cylinder wall. The pressure urging the rails 60, 61 against the cylinder wall is controlled by the oircurnferentially compressible coil spring 50 located to bear against the cylindrical wall .1 of the backing ring. Suflicient clearance exists between the inside of flanges 2 and 3 and the outside of coil spring 50 to allow the spring 50 to float and find its own seat on the cylindrical wall 1. Attention is specifically directed to the aperture 14 in the backing ring 40 which exposes a view of the operating side of the coil spring 50 against the surface of the cylindrical wall 1. From this view, it will be observed that the edges of the aperture do not interfere with relative circumferential movement between the coil spring 50 at the surface of the cylindrical wall 1. This is due to the fact that the edges of the aperture are either inclined opposite to the direction of the lay of the coils of the spring 50 or at an angle greater than the lay of the coils of the spring 50. In either case, the coils of the spring can readily slide over the edges of the aperture without interference. The same result could be obtained by having the edges of the apertures inclined at an angle slightly less than the angle of lay of the coils of the spring 50. As long as the edges of the apertures, such as 3165, inclusive, are curved, obviously, one or the other condition will prevail, more likely the former than the latter, because the center line of the coil spring 50 and, thus, the line of contact cannot move outwardly as far as the flanges 2 and 3.
Turning now to F1698, there is shown a different form of connector from that shown in FIG. 6. This form of connector is a curved rod 65 of a diameter to slidably fit within the ends of the coil springs 51 and 52 and hold them in abutting relation. At either end of the rod 65, the coils of the coil spring 50', arbitrarily indicated as 66 and 67, are deformed from a circular contour of the spring so as to lie in abutting relation with the ends of the rod 65 preventing it from shifting in either direction and migrating out of position.
The modification of connector 70, shown in FIG. 9, operates in substantially the same way as that of FIG. 8. Rod 70 is of .a diameter to slide within the opposite ends of the coil spring 50' so as to hold the ends 51 and 52 in abutting relation. Since the spring is annular and the rod is straight, the ends of the rod will abut certain of the coils, such as 71 and 72, preventing the rod 70 from migrating out of position so as to allow the ends of the spring SO to overlap.
The modification, shown in FIG. 10, is a curved rod 80, one end of which 81 is .bent at an angle to fit between the coils of the spring 50. Rod 80 will hold the ends 51 and 52 in abutting relation and is prevented from migrating out of position 'by the angular end 81 projecting between the coils. The fact that the rod 80 is curved will prevent it from rotating, and thereby unscrewing itself from its proper position.
The modifications, shown in FIG. 11 to FIG. 13, inclusive, are similar to that shown in FIG. 6. The rod 90 has an intermediate loop 91 and opposite straight ends 92 and 93 which can project into the opposite ends of the coil spring. The loop 91 prevents the rod 90 from migrating out of position during operation of the piston ring assembly.
The connector 100, shown in FIG. 12, has a washer 101 staked in place on the straight wire 102 so as to fix the position of the washer 101. This modification operates the same as that in FIGS. 6 and 11.
In FIG. 13, the connector 110 has a washer 111 fixed in place intermediate the length of the rod 112 by olfsetting loops 113 and 114 on either side of the washer 111. This is an alternative way of forming the modification shown in FIG. 12.
Operation In a piston ring assembly, as constructed according to the above description, the coil spring 50 is selected of proper length so that it will be compressed within the backing ring 40 when the piston ring assembly is in operative condition. The spring will then exert a continuous radial force outwardly against the cylindrical wall 1 of the backing ring, and this radial force in turn will be transmitted to the rails and 61 through the rims 4 and 5, respectively. Any irregularities or departures in the surface of the cylinder wall from true cylindrical shape will in part be compensated by the ability of the backing ring 40 to flex circumferentially thereby moving outwardly or inwardly, as the case may be, to allow the rails 60, 61
to move in or force them out and keep the force applied to the cylinder wall by the ring substantially uniform. During this flexing action of the backing ring, coil spring 50 will compress or expand circumferentially sliding over the cylindrical wall surface 1 of the backing ring 40. Changes in diameter of the cylinder are compensated for by this expansion and contraction, as the case may be, coil spring 50 compressing or expanding circurnferentially to compensate for the changes in diameter of the backing ring and the rails 60, 51. The fact that the coil spring 50 has freedom of movement between the annular radial flanges 2 and 3 minimizes any sliding friction at the bearing surfaces between the cylindrical wall 1 of the backing ring and the outer periphery of the annular coil spring 50 at the bearing surfaces between the coil spring and the backing ring. If there is any resistance to the expansion and contraction of the coil spring 50, the coil spring 50 is free to move along the cylindrical wall 1 to avoid the resistance and thereby maintain a uniform radial force on the backing ring 40.
While the backing ring 40 is radially flexible under the influence of the coil spring 50, it has, nevertheless, the beam strength to resist axial flexing under the load which may be imposed thereon by the friction between the rails 60, 61 and the cylinder wall. The truss-like structure of the cylindrical wall 1 forms a circumferential- 1y extending vertical girder in the annular ring 40 contributing the necessary strength to carry the load of the rails 60, 61 without noticeable deflection whereby the rails 60, 61 are maintained against the radial face of the piston ring groove.
In the modified form of the invention illustrated in FIG. 14, a piston ring assembly is shown utilizing the same backing ring, as heretofore described, and coil spring expander ring 50. Flange 3 of the backing ring supports the rail 61 similar to that shown in FIG. 7, but the upper flange 2 of the backing ring supports a compression ring 122. Both piston rings are supported in a piston ring groove 126 in the piston which piston ring groove is divided by a bridge portion 128 accommodating a section of the compression ring 122 of reduced width. This leaves an annular shoulder 123 in the lower surface of the compression ring 122 which is engaged by the upstanding rim 4 of the backing ring.
In operation, the pressure of the coil spring 50 is transmitted directly to the web 1 of the backing ring and from the backing ring through the upstanding rims 4 and 5 to the toil control ring 61, which is a rail. .Rim 4 engages the annular shoulder 123 of the piston ring 122 in a like manner so that the backing ring transmits the force of the coil spring 50 to both rings 61 and 122 urging them outwardly against the cylinder wall 121. Since the backing ring has little torsional rigidity, the two rings 61 and 122 may move relative to each other in a radial direction without any substantial change in the control force applied by the coil spring 50 to either of these rings. The modifications shown in FIGS. 7 and 14, respectfully, are included for the purpose of illustrating how this type of backing ring and coil spring control may be applied to rings to different types for different purposes.
Changes in and modifications of the construction described may be made without departing from the spirit of my invention or sacrificing its advantages.
Having thus described the invention, what is claimed and desired to be secured by Letters Patent is:
.1. In a piston ring assembly, an expansible and contractible piston ring element comprising, an annular strip of spring metal having in part a generally channel cross-section forming a ring element with cylindrical wall portions and integral annular flanges, said cylindrical wall portions comprising a web portion defining a sinuous strip of metal of substantially constant cross-section and including a series of spaced apertures adjacent each flange, the edges of the apertures in one series overhanging the edges of apertures in the other series to define a plurality of oppositely inclined spaced webs, the respective webs extending beyond the adjacent apertures whereby to provide a truss-like structure of uniform beam strength in one direction and of uniform flexibility in another direction.
2. The piston ring assembly of claim 1 wherein the annular flanges are directed radially inwardly with respect to said piston ring element, and an annular round compression spring in rolling contact with said cylindrical wall portions and arranged to exert a radially outwardly directed force at intermediate portions of said spaced webs.
References Cited in the file of this patent UNITED STATES PATENTS Paton Nov. 12, 1940 2,290,499 Smith July 21, 1942 2,713,527 Hsia-Si Pien July 19, 1955 2,722,467 Olson Nov. 1, 1955 2,779,647 Hamrn Jan. 29, 1957 2,917,353 Baumler Dec. 15, 1959
Claims (1)
1. IN A PISTON RING ASSEMBLY, AN EXPANSIBLE AND CONTRACTIBLE PISTON RING ELEMENT COMPRISING, AN ANNULAR STRIP OF SPRING METAL HAVING IN PART A GENERALLY CHANNEL CROSS-SECTION FORMING A RING ELEMENT WITH CYLINDRICAL WALL PORTIONS AND INTEGRAL ANNULAR FLANGES, SAID CYLINDRICAL WALL PORTIONS COMPRISING A WEB PORTION DEFINING A SINUOUS STRIP OF METAL OF SUBSTANTIALLY CONSTANT CROSS-SECTION AND INCLUDING A SERIES OF SPACED APERTURES ADJACENT EACH FLANGE, THE EDGES OF THE APERTURES IN ONE SERIES OVERHANGING THE EDGES OF APERTURES IN THE OTHER SERIES TO DEFINE A PLURALITY OF OPPOSITELY INCLINED SPACED WEBS, THE RESPECTIVE WEBS EXTENDING BEYOND THE ADJACENT APERTURES WHEREBY TO PROVIDE A TRUSS-LIKE STRUCTURE OF UNIFORM BEAM STRENGTH IN ONE DIRECTION AND OF UNIFORM FLEXIBILITY IN ANOTHER DIRECTION.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US57040A US3099455A (en) | 1960-09-19 | 1960-09-19 | Piston ring assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US57040A US3099455A (en) | 1960-09-19 | 1960-09-19 | Piston ring assembly |
Publications (1)
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US3099455A true US3099455A (en) | 1963-07-30 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US57040A Expired - Lifetime US3099455A (en) | 1960-09-19 | 1960-09-19 | Piston ring assembly |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3695622A (en) * | 1970-12-18 | 1972-10-03 | Sealed Power Corp | Piston ring construction |
US3955823A (en) * | 1974-11-19 | 1976-05-11 | Koppers Company, Inc. | Oil ring assembly |
US4111437A (en) * | 1976-09-08 | 1978-09-05 | Sealed Power Corporation | Oil control ring spacer-expander with improved slip latch |
US4204688A (en) * | 1976-09-08 | 1980-05-27 | Sealed Power Corporation | Oil control ring spacer-expander with improved slip latch |
US4809989A (en) * | 1987-06-05 | 1989-03-07 | Otis Engineering Corporation | Coil spring supported sealing element and device |
DE102011014603A1 (en) * | 2011-03-22 | 2012-09-27 | Federal-Mogul Burscheid Gmbh | Tubular spring for piston ring e.g. oil control ring, of internal combustion engine, has connector whose portion is provided with contour deviating from circumferential curvature that is provided in peripheral region of spring |
US20190049012A1 (en) * | 2017-08-09 | 2019-02-14 | Etagen, Inc. | Reinforced sealing rings |
US11193588B2 (en) * | 2017-08-09 | 2021-12-07 | Mainspring Energy, Inc. | Reinforced sealing rings |
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US2220947A (en) * | 1938-06-30 | 1940-11-12 | Perfect Circle Co | Piston ring |
US2290499A (en) * | 1940-02-16 | 1942-07-21 | Mc Quay Norris Mfg Company | Piston ring |
US2713527A (en) * | 1951-11-01 | 1955-07-19 | Wilkening Mfg Co | Piston ring |
US2722467A (en) * | 1952-12-22 | 1955-11-01 | Sealed Power Corp | Piston ring expander spring |
US2779647A (en) * | 1953-12-10 | 1957-01-29 | Muskegon Piston Ring Co Inc | Piston ring |
US2917353A (en) * | 1957-04-18 | 1959-12-15 | Goetzewerke | Tensioning spring for piston rings |
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1960
- 1960-09-19 US US57040A patent/US3099455A/en not_active Expired - Lifetime
Patent Citations (6)
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US2220947A (en) * | 1938-06-30 | 1940-11-12 | Perfect Circle Co | Piston ring |
US2290499A (en) * | 1940-02-16 | 1942-07-21 | Mc Quay Norris Mfg Company | Piston ring |
US2713527A (en) * | 1951-11-01 | 1955-07-19 | Wilkening Mfg Co | Piston ring |
US2722467A (en) * | 1952-12-22 | 1955-11-01 | Sealed Power Corp | Piston ring expander spring |
US2779647A (en) * | 1953-12-10 | 1957-01-29 | Muskegon Piston Ring Co Inc | Piston ring |
US2917353A (en) * | 1957-04-18 | 1959-12-15 | Goetzewerke | Tensioning spring for piston rings |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3695622A (en) * | 1970-12-18 | 1972-10-03 | Sealed Power Corp | Piston ring construction |
US3955823A (en) * | 1974-11-19 | 1976-05-11 | Koppers Company, Inc. | Oil ring assembly |
US4111437A (en) * | 1976-09-08 | 1978-09-05 | Sealed Power Corporation | Oil control ring spacer-expander with improved slip latch |
US4204688A (en) * | 1976-09-08 | 1980-05-27 | Sealed Power Corporation | Oil control ring spacer-expander with improved slip latch |
US4809989A (en) * | 1987-06-05 | 1989-03-07 | Otis Engineering Corporation | Coil spring supported sealing element and device |
DE102011014603A1 (en) * | 2011-03-22 | 2012-09-27 | Federal-Mogul Burscheid Gmbh | Tubular spring for piston ring e.g. oil control ring, of internal combustion engine, has connector whose portion is provided with contour deviating from circumferential curvature that is provided in peripheral region of spring |
US20190049012A1 (en) * | 2017-08-09 | 2019-02-14 | Etagen, Inc. | Reinforced sealing rings |
US10731759B2 (en) * | 2017-08-09 | 2020-08-04 | Mainspring Energy, Inc. | Reinforced sealing rings |
US11193588B2 (en) * | 2017-08-09 | 2021-12-07 | Mainspring Energy, Inc. | Reinforced sealing rings |
US20220074493A1 (en) * | 2017-08-09 | 2022-03-10 | Mainspring Energy, Inc. | Reinforced sealing rings |
US11746904B2 (en) * | 2017-08-09 | 2023-09-05 | Mainspring Energy, Inc. | Reinforced sealing rings |
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